|March 30, 2010, 08:55||
CFD-Post v12.1 & wing pressure coefficients
Join Date: Jul 2009
Posts: 456Rep Power: 14
I've modelled the flow around a 3-D wing and want to see the pressure coefficient distributions around aerofoil sections at different span-wise positions.
How can this be done in CFD-Post v12.1? I guess I need to make a line around the wing at a specified span-wise location and obtain the Cp data on the line. But I cannot get this to work?
|Thread||Thread Starter||Forum||Replies||Last Post|
|Gas pressure question||Dan Moskal||Main CFD Forum||0||October 24, 2002 22:02|
|pressure gradient term in low speed flow||Atit Koonsrisuk||Main CFD Forum||2||January 10, 2002 11:52|
|ASME CFD Symposium - Call for Papers||Chris R. Kleijn||Main CFD Forum||0||September 8, 1998 08:19|
|ASME CFD Symposium - Call for Papers||Chris R. Kleijn||Main CFD Forum||0||September 3, 1998 08:45|
|pressure. lift and drag coefficients||waqar mahboob||Main CFD Forum||0||July 25, 1998 03:34|